CA2992252A1 - Multi-spool gas turbine engine - Google Patents
Multi-spool gas turbine engine Download PDFInfo
- Publication number
- CA2992252A1 CA2992252A1 CA2992252A CA2992252A CA2992252A1 CA 2992252 A1 CA2992252 A1 CA 2992252A1 CA 2992252 A CA2992252 A CA 2992252A CA 2992252 A CA2992252 A CA 2992252A CA 2992252 A1 CA2992252 A1 CA 2992252A1
- Authority
- CA
- Canada
- Prior art keywords
- shaft
- engine
- drive shaft
- agb
- clutch
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/40—Transmission of power
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/85—Starting
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/428,776 US10738709B2 (en) | 2017-02-09 | 2017-02-09 | Multi-spool gas turbine engine |
US15/428,776 | 2017-02-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2992252A1 true CA2992252A1 (en) | 2018-08-09 |
Family
ID=61198703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2992252A Pending CA2992252A1 (en) | 2017-02-09 | 2018-01-17 | Multi-spool gas turbine engine |
Country Status (4)
Country | Link |
---|---|
US (1) | US10738709B2 (pl) |
EP (1) | EP3361073B1 (pl) |
CA (1) | CA2992252A1 (pl) |
PL (1) | PL3361073T3 (pl) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3058470B1 (fr) * | 2016-11-10 | 2019-05-10 | Safran Aircraft Engines | Turbopropulseur comprenant un generateur de gaz et une boite d'accessoires accouplee a une extremite arriere d'un arbre haute pression du generateur de gaz |
US10563591B2 (en) * | 2018-01-17 | 2020-02-18 | United Technologies Corporation | Systems and methods of low spool power extraction |
GB201807840D0 (en) * | 2018-05-15 | 2018-06-27 | Rolls Royce Plc | Gas turbine engine |
US10934972B2 (en) * | 2018-07-19 | 2021-03-02 | Raytheon Technologies Corporation | Stability margin and clearance control using power extraction and assist of a gas turbine engine |
US11261795B2 (en) | 2018-10-18 | 2022-03-01 | Rolls-Royce North American Technologies, Inc. | Dual mode starter generator |
US11008945B2 (en) | 2018-10-18 | 2021-05-18 | Rolls-Royce North American Technologies, Inc. | Accessory gearbox with oppositely disposed starter/generator and air turbine starter |
US11067006B2 (en) * | 2019-03-05 | 2021-07-20 | Rolls-Royce Corporation | Gas turbine engine system with synchronization features for gearbox operation |
US11408353B2 (en) | 2019-03-28 | 2022-08-09 | Honeywell International Inc. | Auxiliary power unit with plural spool assembly and starter transmission arrangement |
US11193425B2 (en) | 2019-06-19 | 2021-12-07 | Raytheon Technologies Corporation | Gearbox for boost spool turbine engine |
US11300056B2 (en) | 2019-08-29 | 2022-04-12 | Rolls-Royce Corporation | Starting alternatives for gas turbine engines |
US11248523B2 (en) | 2019-11-06 | 2022-02-15 | Raytheon Technologies Corporation | Dual clutch transmission for accessory gearbox drive |
US11668245B2 (en) * | 2020-01-28 | 2023-06-06 | Pratt & Whitney Canada Corp. | Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbine |
US11408340B2 (en) | 2020-05-15 | 2022-08-09 | Pratt & Whitney Canada Corp. | Twin-engine system with electric drive |
US11624319B2 (en) | 2020-05-15 | 2023-04-11 | Pratt & Whitney Canada Corp. | Reverse-flow gas turbine engine with electric motor |
US11384693B2 (en) | 2020-05-15 | 2022-07-12 | Pratt & Whitney Canada Corp. | Through-flow gas turbine engine with electric motor and electric generator |
US20210388732A1 (en) * | 2020-06-15 | 2021-12-16 | Pratt & Whitney Canada Corp. | Hybrid gas turbine engine |
US12037913B2 (en) * | 2020-11-02 | 2024-07-16 | Ge Avio S.R.L. | Electric machine assembly for a turbine engine |
US11591967B2 (en) * | 2020-12-21 | 2023-02-28 | The Boeing Company | Systems and methods for providing mechanical power to an aircraft accessory with a turbine engine |
US20220252008A1 (en) * | 2021-02-08 | 2022-08-11 | General Electric Company | Propulsion system configurations and methods of operation |
US12084195B2 (en) | 2021-04-29 | 2024-09-10 | Hamilton Sundstrand Corporation | Dual drive, dual clutch drive system for an aircraft accessory |
US20230076951A1 (en) * | 2021-09-08 | 2023-03-09 | Rolls-Royce North American Technologies Inc. | Electrically driven redundant fuel and oil pumping system for gas turbine engines |
US20230072590A1 (en) * | 2021-09-08 | 2023-03-09 | Rolls-Royce North American Technologies Inc. | Redundant electrically driven fuel and oil pumping system for gas turbines |
US20230096526A1 (en) * | 2021-09-24 | 2023-03-30 | Pratt & Whitney Canada Corp. | Aircraft power plant with a transmission to drive an electrical machine |
US12044182B2 (en) * | 2022-06-21 | 2024-07-23 | General Electric Company | Shaft power transfer for a multi spool gas turbine engine |
US20240035417A1 (en) * | 2022-07-26 | 2024-02-01 | Rolls-Royce Corporation | Shaft couple for rapid start |
Family Cites Families (75)
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NL69078C (pl) | 1944-01-31 | |||
GB713839A (en) | 1951-07-25 | 1954-08-18 | Albert Enticknap | Improvements in or relating to internal combustion turbines |
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EP0103370A1 (en) | 1982-08-11 | 1984-03-21 | Rolls-Royce Plc | Improvements in or relating to gas turbine engines |
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US6732529B2 (en) * | 2001-11-16 | 2004-05-11 | Pratt & Whitney Canada Corp. | Off loading clutch for gas turbine engine starting |
US6735954B2 (en) | 2001-12-21 | 2004-05-18 | Pratt & Whitney Canada Corp. | Offset drive for gas turbine engine |
DE60313392T2 (de) | 2002-05-16 | 2007-08-09 | Rolls-Royce Plc | Gasturbine |
DE10307374A1 (de) | 2003-02-21 | 2004-09-02 | Alstom Technology Ltd | Verfahren zum Betrieb eines teilgeschlossenen, aufgeladenen Gasturbinenkreislaufs sowie Gasturbinensystem zur Durchführung des Verfahrens |
US6895741B2 (en) | 2003-06-23 | 2005-05-24 | Pratt & Whitney Canada Corp. | Differential geared turbine engine with torque modulation capability |
US20070199331A1 (en) | 2003-09-19 | 2007-08-30 | Maguire Alan R | Power transmission arrangement |
FR2863312B1 (fr) | 2003-12-09 | 2008-07-04 | Snecma Moteurs | Turboreacteur a double corps avec moyen d'entrainement des machines accessoires |
US7055303B2 (en) | 2003-12-22 | 2006-06-06 | Pratt & Whitney Canada Corp. | Gas turbine engine architecture |
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FR2882096B1 (fr) | 2005-02-11 | 2012-04-20 | Snecma Moteurs | Turbomoteur a double corps avec des moyens de prise de mouvement sur les rotors basse pression et haute pression, module de prise de mouvement pour le turbomoteur et procede de montage du turbomoteur |
US7500365B2 (en) | 2005-05-05 | 2009-03-10 | United Technologies Corporation | Accessory gearbox |
US20070022735A1 (en) * | 2005-07-29 | 2007-02-01 | General Electric Company | Pto assembly for a gas turbine engine |
FR2892456B1 (fr) | 2005-10-21 | 2008-01-04 | Hispano Suiza Sa | Dispositif d'entrainement de machines accessoires d'un moteur a turbine a gaz |
FR2892455B1 (fr) | 2005-10-21 | 2008-01-04 | Hispano Suiza Sa | Dispositif d'entrainement de machines auxiliaires d'un turbomoteur a double corps |
FR2894621B1 (fr) | 2005-12-09 | 2011-10-14 | Hispano Suiza Sa | Systeme d'entrainement de machines auxiliaires d'un turbomoteur a double corps |
FR2903451B1 (fr) | 2006-07-07 | 2008-09-12 | Snecma Sa | Turbomoteur avec un alternateur et procede de transmission de mouvement a un alternateur |
EP3128164B1 (en) | 2006-08-22 | 2019-07-10 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine with intermediate speed booster |
US7997085B2 (en) | 2006-09-27 | 2011-08-16 | General Electric Company | Gas turbine engine assembly and method of assembling same |
WO2008044973A1 (en) | 2006-10-13 | 2008-04-17 | Volvo Aero Corporation | A device for and a method of starting a gas turbine engine |
US20080148881A1 (en) | 2006-12-21 | 2008-06-26 | Thomas Ory Moniz | Power take-off system and gas turbine engine assembly including same |
WO2008082336A1 (en) | 2006-12-29 | 2008-07-10 | Volvo Aero Corporation | A power transmission device for a gas turbine engine, an aeroplane and a method for operating a gas turbine engine |
US7942079B2 (en) | 2007-02-16 | 2011-05-17 | Hamilton Sundstrand Corporation | Multi-speed gearbox for low spool driven auxiliary component |
US8104289B2 (en) | 2007-10-09 | 2012-01-31 | United Technologies Corp. | Systems and methods involving multiple torque paths for gas turbine engines |
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US9341121B2 (en) | 2013-12-13 | 2016-05-17 | United Technologies Corporation | Gas turbine engine with intercooling turbine section and intercooling turbine section bypass |
EP3114327B1 (en) | 2014-03-06 | 2020-01-08 | United Technologies Corporation | Gas turbine engine accessory architecture |
FR3022301B1 (fr) | 2014-06-12 | 2016-07-29 | Snecma | Turbomachine comprenant un systeme d'entrainement d'un equipement tel qu'un boitier d'accessoires |
US10094277B2 (en) | 2014-06-20 | 2018-10-09 | United Technologies Corporation | Gas turbine engine configured for modular assembly/disassembly and method for same |
US20160169118A1 (en) * | 2014-12-12 | 2016-06-16 | United Technologies Corporation | Dual tower shaft gearbox for gas turbine engine |
US20160230843A1 (en) | 2015-02-09 | 2016-08-11 | United Technologies Corporation | Gearbox for gas turbine engine |
US10371060B2 (en) | 2015-02-20 | 2019-08-06 | Pratt & Whitney Canada Corp. | Compound engine assembly with confined fire zone |
US20160363055A1 (en) | 2015-06-09 | 2016-12-15 | Rolls-Royce North American Technologies, Inc. | Off-set geared turbofan engine |
EP3135882B1 (en) | 2015-08-26 | 2020-04-15 | Honeywell International Inc. | Transverse mounted accessory gearbox |
US10590854B2 (en) | 2016-01-26 | 2020-03-17 | United Technologies Corporation | Geared gas turbine engine |
GB2550397B (en) | 2016-05-19 | 2018-11-21 | Derwent Aviation Consulting Ltd | A turbo machine comprising a compressor system |
-
2017
- 2017-02-09 US US15/428,776 patent/US10738709B2/en active Active
-
2018
- 2018-01-17 CA CA2992252A patent/CA2992252A1/en active Pending
- 2018-02-09 PL PL18156187T patent/PL3361073T3/pl unknown
- 2018-02-09 EP EP18156187.9A patent/EP3361073B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
PL3361073T3 (pl) | 2021-10-11 |
US20180223740A1 (en) | 2018-08-09 |
EP3361073B1 (en) | 2021-03-31 |
EP3361073A1 (en) | 2018-08-15 |
US10738709B2 (en) | 2020-08-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request |
Effective date: 20230113 |